What was found
ON TAKEOFF, NR 2 ENGINE DID NOT REACH T/O, N1 WITH THROTTLE ALIGNED WITH NR1 AND NR3. THROTTLE WAS MOVED SLIGHTLY FWD MANUALLY, AND N1 ROLLED BACK. ENGINE FAIL LIGHT ILLUMINATED, TAKEOFF REJECTED AT 85KTS. INSTALLED FUEL PUMP/MEC IAW MM 73-20-01-2. PERFOMED STEPS B 1-29. STEP 29 C/W IAW MM 75-31-01-5. ACCOMPLISHED LEAK CHECK, IDLE CHECK AND FLIGHT IDLE CHECK, ADJUSTED FLIGHT IDLE 1 TURN CLOCKWISE, THEN ACCOMPLISHED THE MAXIMUM POWER ASSURANCE CHECK/RUN PER MM 71-00-00-5 AND JRH.. ALL PARAMETERS FOUND TO BE WITHIN LIMITS MPA FORM FAXED TO MOCC. NR 2 ENGINE COWLING AND WORK PLATFORM CLOSED AND SECURED PER 71-00-00-2.